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The effect of Mach number on unstable disturbances in shock/boundary-layer interactions

Yao, Yufeng; Krishnan, L.; Sandham, N.D.; Roberts, G.

Authors

Yufeng Yao Yufeng.Yao@uwe.ac.uk
Professor in Aerospace Engineering

L. Krishnan

N.D. Sandham

G. Roberts



Citation

Yao, Y., Krishnan, L., Sandham, N., & Roberts, G. (2007). The effect of Mach number on unstable disturbances in shock/boundary-layer interactions. Physics of Fluids, 19(5), https://doi.org/10.1063/1.2720831

Journal Article Type Article
Publication Date May 1, 2007
Journal Physics of Fluids
Print ISSN 1070-6631
Publisher AIP Publishing
Peer Reviewed Peer Reviewed
Volume 19
Issue 5
DOI https://doi.org/10.1063/1.2720831
Keywords mach number, shock waves, flow instability, boundary layer turbulence, flow simulation, flow separation, bubbles, two-phase flow, white noise, convection, hypersonic flow, Navier-Stokes equations, shear turbulence, numerical analysis, small-amplitude dist
Public URL https://uwe-repository.worktribe.com/output/1028392
Publisher URL http://dx.doi.org/10.1063/1.2720831


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